ICAO Standard Phraseology a Quick Reference Guide for Commercial
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Inter-American Telecommunication Commission
INTER-AMERICAN TELECOMMUNICATION COMMISSION The Inter-American Telecommunication Commission (CITEL) is an entity of the Organization of American States, established by the General Assembly AG/RES.1224(XXII-O/93), in accordance with Article 52 of the Charter of the Organization. CITEL has technical autonomy in the performance of its functions, within the limits of the Charter of the Organization, its Statute, and the mandates of the General Assembly of the Organization. Structure of CITEL a. The CITEL Assembly; b. The Permanent Executive Committee (COM/CITEL); c. The Permanent Consultative Committees; and d. The Executive Secretariat. The objectives of CITEL are to serve as the principal advisory body of the Organization in all matters related to telecommunications in the Americas, to facilitate and promote, by all means available to it, the continuing development of telecommunications in this hemisphere and to consider any other matters relating to Inter-American cooperation in the field of telecommunications as requested by the General Assembly, or the Councils of the Organization. Membership All the Member States of the Organization are Members of CITEL. In addition, other American States which are not members of the Organization are eligible for membership in CITEL and they are only required to submit a request to the CITEL Assembly and the General Assembly of the Organization. Any recognized operating agency or scientific or industrial organization or financial or development institution related to the telecommunications industry, with the approval of the corresponding Member State of CITEL, may become an Associate Member of a Permanent Consultative Committee. Associate Members may fully participate in all the activities of that Permanent Consultative Committee, with voice but without vote. -
E6bmanual2016.Pdf
® Electronic Flight Computer SPORTY’S E6B ELECTRONIC FLIGHT COMPUTER Sporty’s E6B Flight Computer is designed to perform 24 aviation functions and 20 standard conversions, and includes timer and clock functions. We hope that you enjoy your E6B Flight Computer. Its use has been made easy through direct path menu selection and calculation prompting. As you will soon learn, Sporty’s E6B is one of the most useful and versatile of all aviation computers. Copyright © 2016 by Sportsman’s Market, Inc. Version 13.16A page: 1 CONTENTS BEFORE USING YOUR E6B ...................................................... 3 DISPLAY SCREEN .................................................................... 4 PROMPTS AND LABELS ........................................................... 5 SPECIAL FUNCTION KEYS ....................................................... 7 FUNCTION MENU KEYS ........................................................... 8 ARITHMETIC FUNCTIONS ........................................................ 9 AVIATION FUNCTIONS ............................................................. 9 CONVERSIONS ....................................................................... 10 CLOCK FUNCTION .................................................................. 12 ADDING AND SUBTRACTING TIME ....................................... 13 TIMER FUNCTION ................................................................... 14 HEADING AND GROUND SPEED ........................................... 15 PRESSURE AND DENSITY ALTITUDE ................................... -
Mandatory Call Sign Lesson Get Ready for STARBASE in 10 Steps!
Get Ready for STARBASE – Mandatory Call Sign Lesson Overview During this lesson, students will gain a brief introduction to STARBASE. STARBASE goals and expectations will be reviewed with students. Students will then brainstorm ideas for a call sign that will uniquely identify them during their five days at STARBASE Minnesota Duluth. Pilots and astronauts have call signs to signify themselves as unique individuals and to build team comradery. Call signs are used at STARBASE to allow students (and adults) to creatively express their personalities, build a sense of community, and see themselves in a new light. For example, “Allison” might feel that she is not “good at math” but “Galaxy” might see herself as a future Mars rover programmer. Objectives Students will be able to: - Brainstorm a variety of possible call sign names through guided personal research - Choose a call sign using their research and create a personalized nametag - Recall STARBASE goals, expectations, and consequences through guided class discussion - Identify how they will work as a team at STARBASE through a guided activity Materials - One reusable or five temporary name tags per student (ex. mailing labels) - Markers - List of categories students can use to brainstorm call signs (see attached) - Class registration list to record call signs Get ready for STARBASE in 10 steps! (25 minutes) Introduction 1. Explain the STARBASE program to students: “At STARBASE you will have the opportunity to experience science, technology, engineering, and math (STEM) through a variety of experiments and challenges! Some activities include: coding robots, conducting chemistry experiments, solving engineering challenges, using CAD software to design you own creation, using innovative technology like virtual reality (VR) and 3D printing. -
NORWAY LOCAL SINGLE SKY IMPLEMENTATION Level2020 1 - Implementation Overview
LSSIP 2020 - NORWAY LOCAL SINGLE SKY IMPLEMENTATION Level2020 1 - Implementation Overview Document Title LSSIP Year 2020 for Norway Info Centre Reference 20/12/22/79 Date of Edition 07/04/2021 LSSIP Focal Point Peder BJORNESET - [email protected] Luftfartstilsynet (CAA-Norway) LSSIP Contact Person Luca DELL’ORTO – [email protected] EUROCONTROL/NMD/INF/PAS LSSIP Support Team [email protected] Status Released Intended for EUROCONTROL Stakeholders Available in https://www.eurocontrol.int/service/local-single-sky-implementation- monitoring Reference Documents LSSIP Documents https://www.eurocontrol.int/service/local-single-sky-implementation- monitoring Master Plan Level 3 – Plan https://www.eurocontrol.int/publication/european-atm-master-plan- Edition 2020 implementation-plan-level-3 Master Plan Level 3 – Report https://www.eurocontrol.int/publication/european-atm-master-plan- Year 2020 implementation-report-level-3 European ATM Portal https://www.atmmasterplan.eu/ STATFOR Forecasts https://www.eurocontrol.int/statfor National AIP https://avinor.no/en/ais/aipnorway/ FAB Performance Plan https://www.nefab.eu/docs# LSSIP Year 2020 Norway Released Issue APPROVAL SHEET The following authorities have approved all parts of the LSSIP Year 2020 document and the signatures confirm the correctness of the reported information and reflect the commitment to implement the actions laid down in the European ATM Master Plan Level 3 (Implementation View) – Edition 2020. Stakeholder / Name Position Signature and date Organisation -
The Difference Between Higher and Lower Flap Setting Configurations May Seem Small, but at Today's Fuel Prices the Savings Can Be Substantial
THE DIFFERENCE BETWEEN HIGHER AND LOWER FLAP SETTING CONFIGURATIONS MAY SEEM SMALL, BUT AT TODAY'S FUEL PRICES THE SAVINGS CAN BE SUBSTANTIAL. 24 AERO QUARTERLY QTR_04 | 08 Fuel Conservation Strategies: Takeoff and Climb By William Roberson, Senior Safety Pilot, Flight Operations; and James A. Johns, Flight Operations Engineer, Flight Operations Engineering This article is the third in a series exploring fuel conservation strategies. Every takeoff is an opportunity to save fuel. If each takeoff and climb is performed efficiently, an airline can realize significant savings over time. But what constitutes an efficient takeoff? How should a climb be executed for maximum fuel savings? The most efficient flights actually begin long before the airplane is cleared for takeoff. This article discusses strategies for fuel savings But times have clearly changed. Jet fuel prices fuel burn from brake release to a pressure altitude during the takeoff and climb phases of flight. have increased over five times from 1990 to 2008. of 10,000 feet (3,048 meters), assuming an accel Subse quent articles in this series will deal with At this time, fuel is about 40 percent of a typical eration altitude of 3,000 feet (914 meters) above the descent, approach, and landing phases of airline’s total operating cost. As a result, airlines ground level (AGL). In all cases, however, the flap flight, as well as auxiliarypowerunit usage are reviewing all phases of flight to determine how setting must be appropriate for the situation to strategies. The first article in this series, “Cost fuel burn savings can be gained in each phase ensure airplane safety. -
TCAS II) by Personnel Involved in the Implementation and Operation of TCAS II
Preface This booklet provides the background for a better understanding of the Traffic Alert and Collision Avoidance System (TCAS II) by personnel involved in the implementation and operation of TCAS II. This booklet is an update of the TCAS II Version 7.0 manual published in 2000 by the Federal Aviation Administration (FAA). It describes changes to the CAS logic introduced by Version 7.1 and updates the information on requirements for use of TCAS II and operational experience. Version 7.1 logic changes will improve TCAS Resolution Advisory (RA) sense reversal logic in vertical chase situations. In addition all “Adjust Vertical Speed, Adjust” RAs are converted to “Level-Off, Level-Off” RAs to make it more clear that a reduction in vertical rate is required. The Minimum Operational Performance Standards (MOPS) for TCAS II Version 7.1 were approved in June 2008 and Version 7.1 units are expected to be operating by 2010-2011. Version 6.04a and 7.0 units are also expected to continue operating for the foreseeable future where authorized. 2 Preface................................................................................................................................. 2 The TCAS Solution............................................................................................................. 5 Early Collision Avoidance Systems................................................................................ 5 TCAS II Development .................................................................................................... 6 Initial -
An Analysis of En Route Controller- DOT-VNTSC-FAA-93-2 Pilot Voice Communications Research and Development Service Washington
DOT/FAA/RD-93/11 An Analysis of En Route Controller- DOT-VNTSC-FAA-93-2 Pilot Voice Communications Research and Development Service Washington. DC 20591 Kim M. Cardosi Research and Special Programs Administration John A. Volpe National Transportation Systems Center Cambridge, MA 02142-1093 Final Report March 1993 Reprint July 1993 This document is available to the public through the National Technical Information Service, Springfield. VA22161 © U.S.Department ofTransportation Federal Aviation Administration NOTICE This document is disseminated under the sponsorship of the Departmentof Transportation inthe interest of information exchange. The United States Government assumesno liability forits contents orusethereof. NOTICE The United States Government does not endorse products ormanufacturers. Trade ormanufacturers' names appear herein solely because they are considered essential to the object ofthis report. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 STSiedS1"^txa neeoea, ano the — or any other - Headquarters ,, Arlington. VA REPORT TYPE ANO DATES COVERED Final Report 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS An Analysis of En Route Controller-Pilot Voice Communications FA3L1/A3021 6. AUTHOR(S) Kim H. Cardosi 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION John A. Volpe National Transportation Systems Center REPORT NUMBER Research and Development Administration Transportation Systems Center DOT-VNTSC-FAA-93-2 Cambridge, MA 02142 9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/MONITORING Federal Aviation Administration AGENCY REPORT NUMBER Research and Development Service 800 Independence Ave., S.W. DOT/FAA/RD-93/11 Washington, DC 20591 11. SUPPLEMENTARY NOTES 12a. DISTRIBUTION/AVAILABILITY STATEMENT 12b. DISTRIBUTION CODE This document is available to the public through the National Technical Information Service, Springfield, VA 22161 13. -
Frequencies Between Serial Killer Typology And
FREQUENCIES BETWEEN SERIAL KILLER TYPOLOGY AND THEORIZED ETIOLOGICAL FACTORS A dissertation presented to the faculty of ANTIOCH UNIVERSITY SANTA BARBARA in partial fulfillment of the requirements for the degree of DOCTOR OF PSYCHOLOGY in CLINICAL PSYCHOLOGY By Leryn Rose-Doggett Messori March 2016 FREQUENCIES BETWEEN SERIAL KILLER TYPOLOGY AND THEORIZED ETIOLOGICAL FACTORS This dissertation, by Leryn Rose-Doggett Messori, has been approved by the committee members signed below who recommend that it be accepted by the faculty of Antioch University Santa Barbara in partial fulfillment of requirements for the degree of DOCTOR OF PSYCHOLOGY Dissertation Committee: _______________________________ Ron Pilato, Psy.D. Chairperson _______________________________ Brett Kia-Keating, Ed.D. Second Faculty _______________________________ Maxann Shwartz, Ph.D. External Expert ii © Copyright by Leryn Rose-Doggett Messori, 2016 All Rights Reserved iii ABSTRACT FREQUENCIES BETWEEN SERIAL KILLER TYPOLOGY AND THEORIZED ETIOLOGICAL FACTORS LERYN ROSE-DOGGETT MESSORI Antioch University Santa Barbara Santa Barbara, CA This study examined the association between serial killer typologies and previously proposed etiological factors within serial killer case histories. Stratified sampling based on race and gender was used to identify thirty-six serial killers for this study. The percentage of serial killers within each race and gender category included in the study was taken from current serial killer demographic statistics between 1950 and 2010. Detailed data -
Using an Autothrottle to Compare Techniques for Saving Fuel on A
Iowa State University Capstones, Theses and Graduate Theses and Dissertations Dissertations 2010 Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft Rebecca Marie Johnson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/etd Part of the Electrical and Computer Engineering Commons Recommended Citation Johnson, Rebecca Marie, "Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft" (2010). Graduate Theses and Dissertations. 11358. https://lib.dr.iastate.edu/etd/11358 This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Using an autothrottle to compare techniques for saving fuel on A regional jet aircraft by Rebecca Marie Johnson A thesis submitted to the graduate faculty in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Major: Electrical Engineering Program of Study Committee: Umesh Vaidya, Major Professor Qingze Zou Baskar Ganapathayasubramanian Iowa State University Ames, Iowa 2010 Copyright c Rebecca Marie Johnson, 2010. All rights reserved. ii DEDICATION I gratefully acknowledge everyone who contributed to the successful completion of this research. Bill Piche, my supervisor at Rockwell Collins, was supportive from day one, as were many of my colleagues. I also appreciate the efforts of my thesis committee, Drs. Umesh Vaidya, Qingze Zou, and Baskar Ganapathayasubramanian. I would also like to thank Dr. -
Advisory Circular (AC)
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Parts 91, 121, 125, and 135 Date: 7/30/12 AC No: 120-74B Flightcrew Procedures During Taxi Initiated by: Change: Operations AFS-200/800 1. PURPOSE. This advisory circular (AC) provides guidelines for the development and implementation of standard operating procedures (SOP) for conducting safe aircraft operations during taxiing to avoid causing a runway incursion. In accordance with Federal Aviation Administration (FAA) Order 7050.1, Runway Safety Program, the definition of a runway incursion is any occurrence at an aerodrome involving the incorrect presence of an aircraft, vehicle, or person on the protected area of a surface designated for the landing and takeoff of aircraft. It is intended for use by persons operating aircraft with two or more pilots on the flight deck under Title 14 of the Code of Federal Regulations (14 CFR) parts 91, 121, 125, and 135. The FAA recommends that these guidelines become an integral part of all SOPs, flight operations manuals (FOM), and formal flightcrew member training programs. The use of flightcrew SOPs should be emphasized and employed during all phases of flight, including ground operations. Appendices 1 and 2 of this AC contain examples of SOPs that are identical or similar to some SOPs currently in use. These appendices are not directive or prescriptive in nature and do not represent a rigid FAA view of Best Practices. SOPs may vary among fleets and among certificate holders and may change over time. Operators may integrate the information contained in Appendices 1 and 2 into their fleet-specific, route-specific, and equipment-specific operations and checklists. -
N87- 19393 CE Bith Ab AUTCEETIC TESMINAL EM (BASA) 21 P CSCL 17Ti Unclas H1/06 43501 NASA Tech Ni Ca I Paper 2669
) A SIPSCLATICL EVALUATION GP A N87- 19393 CE bITH Ab AUTCEETIC TESMINAL EM (BASA) 21 p CSCL 17ti Unclas H1/06 43501 NASA Tech ni ca I Paper 2669 1987 A Simulation Evaluation of a Pilot Interface With an Automatic Terminal Approach System David A. Hinton Langley Research Center Hampt o n, Virginia National Aeronautics and Space Administration Scientific and Technical Information Branch Summary with a high potential for mistakes and has limited time to detect and correct any errors. A successful A piloted-simulation study was performed to arrival depends on the correct interpretation of ap- evaluate the pilot interface with an automatic termi- proach chart details, the correct setting of numerous nal approach system (ATAS). The ATAS was con- cockpit controls, and precise aircraft guidance near ceived as a concept for improving the pilot inter- the ground. face with high levels of automation. It consists of Automation in the form of an autopilot has been instrument approach data storage, automatic radio used to reduce pilot work load and improve pilot tuning, autopilot, autothrottle, and annunciation of performance in the terminal area. Research studies These components allow the ATAS flight status. (ref. 2) and airplane accident and incident reports to automatically execute instrument approaches, in- suggest, however, that the probability of pilot error cluding procedure turns, altitude changes, missed actually increases with an increase in automation, approaches, and holding patterns, without requir- partially because of design limitations of the pilot- ing the pilot to set up navigation radios or change machine interface. Conventional autopilot interfaces autopilot modes. provide the pilot with many opportunities to make The results show that fewer pilot blunders were errors because of the requirements to change radio made during approaches when using the ATAS than frequencies and autopilot modes as the approach when using a baseline, heading-select autopilot. -
CRUISE FLIGHT OPTIMIZATION of a COMMERCIAL AIRCRAFT with WINDS a Thesis Presented To
CRUISE FLIGHT OPTIMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS _______________________________________ A Thesis presented to the Faculty of the Graduate School at the University of Missouri-Columbia _______________________________________________________ In Partial Fulfillment of the Requirements for the Degree Master of Science _____________________________________________________ by STEPHEN ANSBERRY Dr. Craig Kluever, Thesis Supervisor MAY 2015 The undersigned, appointed by the dean of the Graduate School, have examined the thesis entitled CRUISE FLIGHT OPTMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS presented by Stephen Ansberry, a candidate for the degree of Master of Science, and hereby certify that, in their opinion, it is worthy of acceptance. Professor Craig Kluever Professor Roger Fales Professor Carmen Chicone ACKNOWLEDGEMENTS I would like to thank Dr. Kluever for his help and guidance through this thesis. I would like to thank my other panel professors, Dr. Chicone and Dr. Fales for their support. I would also like to thank Steve Nagel for his assistance with the engine theory and Tyler Shinn for his assistance with the computer program. ii TABLE OF CONTENTS ACKNOWLEDGEMENTS………………………………...………………………………………………ii LIST OF FIGURES………………………………………………………………………………………..iv LIST OF TABLES…………………………………………………………………………………….……v SYMBOLS....................................................................................................................................................vi ABSTRACT……………………………………………………………………………………………...viii 1. INTRODUCTION.....................................................................................................................................1